Aviation sector
2021-09-26
Replacing nickel-based superalloys with SiCf/SiC ceramic matrix composites achieves a 60% weight reduction, a 200°C increase in service temperature, reduced cooling‑air consumption, and an improved thrust‑to‑weight ratio.
Replacing nickel-based superalloys with SiCf/SiC ceramic matrix composites achieves a 60% weight reduction, a 200°C increase in service temperature, reduced cooling‑air consumption, and an improved thrust‑to‑weight ratio.
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